N880AS

Service difficulty reports · 192

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N880AS' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASOA2014052310580Skin · corrodedRIGHT OVERWING EMERGENCY EXIT DOOR INNER SKIN CORRODED INSIDE BOTTOM OF DOOR. REMOVED 2 CORRODED ANGLES IAW SRM 51-42-06. INSTALLED 2 NEW ANGLES, PN 601R31123-108 AND 107 IAW DWG 601R31123, REV H AND SRM 51-42-06.May 1, 2014 · N880AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA2014052310579Skin · crackedLT LOWER WING PLANK CRACKED APP 1" AT 148.019. COMPLIED WITH ECTC REO 601R-57-21-130 AND GREO 601R-57-21-130, REV K.May 1, 2014 · N880AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014052310578Bulkhead · chafedFOUND REAR PRESSURE BULKHEAD WEB HAS THREE CHAFED AREAS APPROX .200 INCH LONG BY .200 INCH WIDE .003 INCH DEEP AT RBL 18.00, RBL 27.50 AND RBL 36.20 WL 105. COMPLIED WITH ECTC REO 601R-53-61-2155.May 1, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014052310577Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATIONS NOTED AT LBL 27.50, WL 130, APPROXIMATELY .2 INCHES IN LENGTH, 90 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO: 601R-53-61-1541.May 1, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014052310576Skin · chafedLEFT AILERON UPPER L/E IS CHAFED AT MULTIPLE LOCATIONS. REMOVED DAMAGED UPPER L/E SKIN FROM LT AILERON IAW SRM 51-42-06, REV 32. FITTED, DRILLED, AND INSTALLED NEW UPPER L/E SKIN IAW SRM 51-40-11, 51-42-06, 51-42-13.May 1, 2014 · N880AS · Cndair CL6002B19 · AileronsSDR ASOA2014052310575Bracket · crackedLEFT WING TO FUSELAGE FAIRING BRACKET AT BS 449.85 IS CRACKED. R & R THE FAIRING BRACKET WITH NEW IAW SRM 51-40-11, 51-42-06 AND 51-45-00.May 1, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052310574Bracket · crackedRT WING TO FUSELAGE FAIRING BRACKET AT BS 449.85 - 461 ARE CRACKED. R & R RT WING TO FUSELAGE FAIRING BRACKET IAW SRM 51-42-06, REV 32.May 1, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052310573Arm · gougedFOUND GOUGE ON RT OTBD FLAP CENTER HINGE ARM WS 220.00 BOTTOM INBD MOUNTING LUG. BLENDED GOUGE IAW EA:26-2014-048, REV. ORIGINAL. PERFORMED SHOT PEENING ON THE REQUIRED SURFACE RT OTBD FLAP CENTER HINGE LUG IAW EA 26-2014-048, STEP 3.May 1, 2014 · N880AS · Cndair CL6002B19 · Trailing Edge FlapsSDR ASOA2013121809657Detector · failedDISPLAY COOL MESSAGE IN FLIGHT. COMPLIED WITH QRH. MESSAGE WOULD NOT EXTINGUISH. ACFT RETURNED TO DEPARTURE. INSPECTED DUCT WORK TO FANS. NO DEFECTS NOTED. R & R DIPSLAY COOLING FILTER IAW AMM 21-24-15. NO DEFECTS NOTED. R & R LOW FLOW DETECTOR IAW AMM Dec 3, 2013 · N880AS · Cndair CL6002B19 · Air Distribution SystemSDR ASOA2013092509095Lamp · burned outEMERGENCY LIGHT FWD OF THE PAX DOOR INOP. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.Sep 23, 2013 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012082002081Connector · disconnectedWARDROBE AND GALLEY EMERGENCY LIGHTS ARE INOPERATIVE. TROUBLESHOT EMERGENCY LIGHTS IAW WDM 33-51-00. FOUND FOUR QUICK DISCONNECT CONNECTORS DISCONNECTED. SWAPED AT LT FWD FLOOR LEVEL EXIST FLOODLIGHT (DS9LY) AND FWD EXIT SIGN (DS10LY). CONNECTED IS9LY AND DSAug 20, 2012 · N880AS · Cndair CL6002B19 · Light System WiringSDR ASOA2012081602074Attach Fitting · corrodedPAX DOOR UPPER HINGE SECTION AT FS 320.10 & FS 338.00 BOTH FWD 7 AFT CLEAT CORRODED BEYOND LIMITS. REMOVED CORRODED CLEAT. FITTED, DRILLED & INSTALLED NEW CLEAT IAW SRM 51-42-06 & 51-42-13.Aug 1, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA2012081602073Attach Angle · crackedATTACH ANGLE ON FWD OF ENGINE SUPPORT BEAM AT FS 635.30 BL, RBL 27.50 HAS A .3" CRACK IN LOWER CORNER. FAILED VISUAL NDT INSPECTION. REMOVED CRACKED ATTACH ANGEL FWD OF ENGINE SUPPORT BEAM IAW SRM 51-42-06 AND 51-42-21. REPLACED CRACKED ATTACH ANGLE IAW SRM Jul 31, 2012 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2012081602072Attach Angle · crackedCLIP, ON FWD OF ENGINE SUPPORT BEAM AT FS 635.30 BL, RBL 18.00 HAS A .5" CRACK IN LOWER CORNER. FAILED VISUAL NDT INSPECTION. REMOVED CRACKED CLIP AT FS 635.30 BL, RBL 18.00 IAW SRM 51-42-21. REPLACED CRACKED WITH NEW CLIP IAW SRM 51-42-21.Jul 31, 2012 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2012080102022Attach Bracket · crackedCARGO BAY, AFT BRACKET AT FS 621 CRACKED WHERE BRACKET ATTACHES TO CROSSMEMBER CARGO DOOR. R & R CARGO BAY AFT BRACKET IAW SRM 51-42-21-00.Jul 27, 2012 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2012080102014Seat Track · corrodedIN PASSENGER COMPARTMENT, RT SIDE SEAT TRACK AFT OF FS 409+128 IS CORRODED SEVERAL LOCATIONS. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV A.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012082002080Angle · corrodedFS 280.00 BETWEEN LBL 9.00 TO RBL 9.00, FWD AND AFT J ANGLES ARE CORRODED. REMOVED ANGLE IAW SRM 51-42-06, 51-42-21. LOCATED NEW ANGLE IAW SRM 51-40-11. INSTALLED NEW ANGLE IAW SRM 51-42-06 AND 51-42-21.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012081602071Web · corrodedIN PASSENGER COMPARTMENT AT FS 559.00, RBL 42.900 FLOOR SUPPORT FINGER WEB IS CORRODED.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012081602070Floor Support · corrodedIN PASSENGER COMPARTMENT FLOOR SUPPORT BETWEEN FS 424.00 TO FS 559.00 RBL 42.00, AROUND FLOORBOARD ATTACHMENT HOLES, FLOOR SUPPORT CORRODED. COMPLIED WITH ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012081602069Floor Support · corrodedPASSENGER COMPARTMENT AT FS 559.00, LBL 36.00 FLOOR SUPPORT FINGER WEB IS CORRODED.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012081602068Seat Track · corrodedPASSENGER COMPARTMENT LT SIDE WALL SEAT TRACK AT FS 399.00 IS CORRODED. REPAIRED LT SIDEWALL SEAT TRACK IAW REO 601R-53-00-55. ECTC REQUIRED.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012081602067Floor Support · crackedIN PASSENGER COMPARTMENT, FLOOR STRUCTURE AT FS 280.00 RBL 9.00 OTBD ATTACHMENT ANGLE IS CRACKED. REPAIRED IAW REO 601R-53-11-926, REV B.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012080102021Seat Track · corrodedPASSENGER COMPARTMENT SEAT TRACK AT FS 409+112 TO 559, RBL 9.00 IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. DRILLED AND COUNTERSUNK NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102020Seat Track · corrodedIN PASSENGER COMPARTMENT SEAT TRACK, FS 409+112 TO 559, LBL 9.00 IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. DRILLED AND COUNTERSUNK NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102019Seat Track · corrodedIN PASSENGER COMPARTMENT, RBL 9 BETWEEN FS 396 TO 409+120, SEAT TRACK IS CORRODED AT BS 409. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802 & LOCATED & DRILLED NEW SERVICEABLE TRACK IAW SRM 51Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102018Seat Track · corrodedIN PASSENGER COMPARTMENT, LBL 9.00 FS 396 TO 409+120, SEAT TRACK IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED IAJul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102017Seat Track · corrodedIN PASSENGER COMPARTMENT, RBL 9.900 BETWEEN FS 364 TO 399, SEAT TRACK IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102016Seat Track · corrodedIN PASSENGER COMPARTMENT LBL 9.00 BETWEEN FS 364 TO FS 399, SEAT TRACK CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED CORRODED SEAT TRACK & INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102015Seat Track · corrodedIN PASSENGER COMPARTMENT RT SIDE SEAT TRACK AFT OF FS 409+128 IS CORRODED AT SEVERAL LOCATIONS. COMPLIED WITH EC/TC REO 601R-53-00-55 AND REO 601R-53-00-055, REV A.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102013Seat Track · corrodedIN PASSENGER COMPARTMENT RT SIDEWALL SEAT TRACK AT FS 409+8 CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055. RII FOUND TO BE SATISFACTORY.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012073002000Frame · crackedFS 718 FRAME, CRACKED JUST BELOW STRINGER 11 RT. REMOVED DAMAGE IAW REO 601R-53-61-193. PERFORMED LPI CUT LINE IAW NDTM 51-10-08. NO INDICATIONS NOTED.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2012073001999Angle · crackedPASSENGER COMPARTMENT FLOOR STRUCTURE AT FS 484.00, LBL 27.00, ATTACHMENT ANGLE IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. REPLACED CRACKED ANGLE AT FS 494.00, LBL 27.00 IAW SRM 51-42-21 AND SRM 51-42-06 PN 601R31171-17. TJul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012081602066Angle · crackedFS 625 OBLIQUE LT CRACKED. REMOVED CRACKED OBLIQUE ANGLE COMMON TO LT SIDE FS 625 AND REPLACED IT WITH NEW PART IAW SRM 51-42-21.Jul 24, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012071101887Charger · unserviceableALL EMERGENCY LIGHTS ON NR 2 BATTERY INOPERATIVE. R & R NR 2 BATTERY AND BATTERY CHARGER IAW AMM 33-51-04 AND AMM 33-51-05, OPS CHECKED GOOD.Jul 7, 2012 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201201779Potentiometer · out of adjustON ARRIVAL, SELECTED FLAPS TO 8, FLAPS DID NOT MOVE. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. PERFORMED POTENTIOMETER ADJUSTMENT OF THE FECU IAW AMM 27-51-10-830-008. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AND R & R RT FLAP BPSU IAW 27-51-10. Jun 8, 2012 · N880AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA201201562Flap System · failedFLAPS FAIL CAUTION MESSAGE- FLAPS FAILED AT 0 DEGREES. EMERGENCY DECLARED, COMPLIED WITH AD 2009-06-12. NO FURTHER DEFECT NOTED.May 4, 2012 · N880AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA201201287Lamp · burned outNR 8 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 8 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Apr 16, 2012 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201102196Latch · malfunctionedDESCENDING THROUGH FL180, WE HAD A PASSENGER DOOR WARNING MESSAGE. RAN QRH WE UNPRESSURIZED THE ACFT. DOOR HANDEL POPPED UP, WE DID NOT ATTEMPT TO RESTOW. GREEN INDICATORS WENT RED (EMERGENCY DECLARED AS A PRECAUTION) REPAIRED INNER DOOR LATCH MECHANISMNov 15, 2011 · N880AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101758Light · brokenMAIN ENTRANCE EMERGENCY LIGHT ASSY BROKEN. R & R MAIN ENTRANCE EMERGENCY LIGHT ASSY IAW AMM 33-51-01.Sep 18, 2011 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201100956Warning System · false activationLT ENG OIL PRESSURE MESSAGE JUST PRIOR TO LANDING WITH SMOKE REPORTED TRAILING FROM THE ACFT BY THE TOWER. (EMERGENCY DECLARED AND FIRE TRUCKS ROLLED AS A PRECAUTION) PERFORMED OPS CHECK AT LOW POWER AND HIGH POWER ENGINE RUN, OPS CHECK GOOD IAW AMM 71-00-00,May 7, 2011 · N880AS · Cndair CL6002B19 · Central WarningSDR ASOA201100811Lamp · burned outFUSELAGE EXTERNAL EMERGENCY LIGHT IN FRONT OF LEFT EMERGENCY EXIT INOP. RELAMPED LEFT NR 3 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD. RELAMPED LEFT NR 3 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD.Apr 24, 2011 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001095Lamp · burned outNR 1 EMERGENCY LIGHT FWD OF PAX DOOR INOP. RELAMPED NR 1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. RELAMPED NR 1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. (CLOSED)Aug 11, 2010 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201000366Lens · crackedJOB 8760611 OPERATION 412 / PNL 232DZ EXIT SIGN HSG AND LENS COVER CRACKED. R & R EXIT SIGN HSG AND LENS COVER ON PNL 232DZ IAW MM 33-51-13-000-801 AND 33-51-13-400-801. OPS CHECK DUE. OPS CHECK OF THE EMERGENCY LIGHTS GOOD IAW AMM 33-51-00-710-801.Mar 2, 2010 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201000280Intercostal · corrodedINTERCOSTAL BETWEEN FS 333.0 AND 349.0 AT STR 25R CORRODED. REMOVED AND REPLACED INTERCOSTAL AT STR 25R IAW SRM 51-42-06 STEPS 9,10 & 11.Feb 19, 2010 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000258Floorbeam · crackedWHILE REPLACING THE CARGO FLOOR FILLPLATE ON THE LT SIDE FS 564-621, FOUND THE FS 605 FLOORBEAM TO BE CRACKED, DENTED, GOUGED AND THE HOLE IS ELONGATED AT LBL42. THE DAMAGE IS ALL AROUND ONE HOLE. REPAIR TO TRAVERSE BEAM COMPLETED IAW REO 601R-53-61-3542 ANDFeb 15, 2010 · N880AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201000257Floorbeam · crackedFS 484.00 RBL 27 OTBD FLOOR SUPPORT ANGLE CRACKED PREVIOUS REPAIRED ANGLE. REPAIR TO THE INTERCOSTAL AT FS 484 BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.Feb 15, 2010 · N880AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201000244Frame · corrodedCORROSION ON FS 349.00 FRAME TO ATTACHMENT FLANGE BETWEEN STR 26L - STR 26R. (3 PLACES). REMOVED FRAME IAW SRM 51-42-06 STEPS A, B1 THROUGH 6 AND SRM 51-42-21 STEPS 11A1 AND B1. LOCATED AND DRILLED NEW FRAME SECTOR IAW AMM 51-42-06. INSTALLED NEW FRAME SECTFeb 15, 2010 · N880AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201000336Filler · crackedAFT FILLER STRIP LBL 27.0, FS 589.0 TO FS 615.00 CRACKED IN NUMEROUS PLACES. SEAT TRACK FILLER STRIP. R & R FILLER STRIP AT LBL 27.0 FS 589.0 TO 615.0 IAW SRM 51-41-00.Feb 10, 2010 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000209Floor Support · corrodedCARGO FLOORBEAM CAP LBL 27.0 F.S. 589.0 TO F.S. 621.0 CORRODED AROUND NUTPLATE HOLES. REMOVED PLASTIC GAP STRIP. REMOVED BOLTS FROM ELEVATOR PULLEY ASSY MOUNT. REMOVED FLOORBEAM CAP IAW SRM 51-42-06, STEP 11 AND SRM 51-42-21, STEP 11. LOCATED, DRILLED & IFeb 10, 2010 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000201Frame · corrodedFUSELAGE FRAME HAS CORROSION FS 333.0 STR 26L TO STR 27. REMOVED FUSELAGE FRAME AT FS 333.00 STR 23L-23R IAW SRM 51-42-06 & 51-42-21. NEW FRAME SECTOR REQUIRES LOCATED, DRILLED, AND INSTALLED. NEW FRAME SECTOR IS LOCATED AND DRILLED IAW 51-42-06 STEP 7 A & Feb 10, 2010 · N880AS · Cndair CL6002B19 · Fuselage Main, Frame
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